US2198771A - Welded two-piece light alloy piston - Google Patents

Welded two-piece light alloy piston Download PDF

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Publication number
US2198771A
US2198771A US264380A US26438039A US2198771A US 2198771 A US2198771 A US 2198771A US 264380 A US264380 A US 264380A US 26438039 A US26438039 A US 26438039A US 2198771 A US2198771 A US 2198771A
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US
United States
Prior art keywords
piston
welded
ring belt
wall
belt area
Prior art date
Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
Expired - Lifetime
Application number
US264380A
Inventor
Ronald M Hazen
Jr Thomas S Mccrae
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Motors Liquidation Co
Original Assignee
Motors Liquidation Co
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Priority claimed from US137656A external-priority patent/US2159989A/en
Application filed by Motors Liquidation Co filed Critical Motors Liquidation Co
Priority to US264380A priority Critical patent/US2198771A/en
Application granted granted Critical
Publication of US2198771A publication Critical patent/US2198771A/en
Anticipated expiration legal-status Critical
Expired - Lifetime legal-status Critical Current

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    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02F—CYLINDERS, PISTONS OR CASINGS, FOR COMBUSTION ENGINES; ARRANGEMENTS OF SEALINGS IN COMBUSTION ENGINES
    • F02F3/00—Pistons 
    • F02F3/0015—Multi-part pistons
    • F02F3/003—Multi-part pistons the parts being connected by casting, brazing, welding or clamping
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02F—CYLINDERS, PISTONS OR CASINGS, FOR COMBUSTION ENGINES; ARRANGEMENTS OF SEALINGS IN COMBUSTION ENGINES
    • F02F3/00—Pistons 
    • F02F3/16—Pistons  having cooling means
    • F02F3/20—Pistons  having cooling means the means being a fluid flowing through or along piston
    • F02F3/22—Pistons  having cooling means the means being a fluid flowing through or along piston the fluid being liquid
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02B—INTERNAL-COMBUSTION PISTON ENGINES; COMBUSTION ENGINES IN GENERAL
    • F02B75/00—Other engines
    • F02B75/02—Engines characterised by their cycles, e.g. six-stroke
    • F02B2075/022—Engines characterised by their cycles, e.g. six-stroke having less than six strokes per cycle
    • F02B2075/025—Engines characterised by their cycles, e.g. six-stroke having less than six strokes per cycle two
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02F—CYLINDERS, PISTONS OR CASINGS, FOR COMBUSTION ENGINES; ARRANGEMENTS OF SEALINGS IN COMBUSTION ENGINES
    • F02F2200/00—Manufacturing
    • F02F2200/04—Forging of engine parts

Definitions

  • pistons which are light, but of adequate strength, while capable of dissipating effectively the heat to which they are subjected.
  • the object of the invention is a strong, light weight piston, capable of quickly dissipating the 16 heat to which it is subjected.
  • Another object of the invention is a piston in which the heat flow to the ring belt is limited.
  • the crown of the piston is supported from the piston pin bosses mainly by a circular strut forming an inner wall, spaced from and of greater section than the outer wall of the piston and providing an annular insulating air space between the two walls.
  • piston is made in two pieces subsequently fastened together by screwed and/or welded joints, or the like.
  • One piece forms one part of the wall of the annular insulating air space and includes the ring belt area and the strut and the other piece forms the remaining part of the wall of the annular insulating air space and includes the remainder of the piston.
  • the two-piece construction permits a greater control and freedom in the choice of section and so in the provision of suitable cooling flns and insulating air spaces.
  • the drawing shows three modifications of a piston according to the invention.
  • Fig. 1 is a view, partly in elevation andpartly in section, of a piston structure according to the invention.
  • Figs. 2 and 3 are views, partly in elevation and partly in section of modifications according to the invention.
  • the piston is provided with diametrically opposite bosses such as I, having bearings 2 for a piston pin (not shown). Integral with the bosses l and above the bosses is a ring b'elt area 3 in which grooves 4 are provided for conventional packing rings (not shown) and a circular strut 5 having an outer diameter such as to leave an annular space 6 between the ring belt area 3 and the strut 5.
  • the piston crown 1 forms the closure for the upper end of the amiular space 6. It has female threads 8 engaging male threads 9 at the top end of the circular strut 5.
  • the peripheral rim III of the piston crown extends to the top edge ll of the piston skirt above the ring belt area 3.
  • the piston structure is completed by screwing the two parts together, after which the joint between the rim ll) of the piston crown and the top edge II is sealed by welding as indicated in the drawing.
  • Fig. 2 The construction according to Fig. 2 is essentially similar to the construction according to Fig. 1, except that the circular strut is female threaded and the piston crown is male threaded.
  • the piston crown I5 is integral with the circular strut l6 and the ring belt area l1.
  • the piston skirt portion I8 is a push fit over the bosses I9 which are integral with the circular strut l6 and the ring belt area I! as in the structure according to Fig. 1.
  • the skirt portion I8 is welded to the ring belt area I! as shown.
  • the annular space extends closer to the outer cylindrical surface of the piston at points above and below the ring belt area in the outer wall of the piston and has at all points a greater cross-sectional area than points above and below the ring belt area.
  • the heat flow from the head of the piston to the ring belt area is restricted by the narrow section of metal between these two parts.
  • the circular strut forming the inner wall of the insulating annular space is sufficiently large to carry the main gas pressure loads and the heat flow directlyon to the piston pin bosses-only a small part of the load and the heat flow being transmitted through the outer section of the piston.
  • the two parts 01' the piston can be made of any suitable light alloy (either forged or cast), and it will be seen that a structure has been provided in which all critical points, as well as the cooling fins, may be completely machined to any desired tolerance limits before assembl We claim:
  • a strut to support the crown from the piston pin bosses and forming an inner wall spaced from the outer wall of the piston to provide an enclosed annular insulating air space be-. tween the ring belt area and the strut forming the inner wall, said inner wall having at all points a greater cross-sectional area than points above and below the ring belt area inthe outer wall of the piston, whereby only small portions oi the gas pressure loads and the heat to which the crown is exposed in an engine cylinder are transmitted to the ring belt area, and the main portions oi.
  • the gas pressure loads and'the heat flow are carried directly through the inner wall to the piston pin bosses, said piston consisting of v a plurality oi pieces fastened together, one of said pieces forming a part. of the wall of the annular insulating air space and including the ring belt area and the strut, there being a Joint in the outer periphery of the piston above the piston pin bosses, between said piece and the remainder of the piston.

Description

April 30. 1940. 'R. 'M. HAZEN ET A]. 2 198,771
WELDED TWO-PIECE LIGHT ALLOY PISTON Original Filed April 19. 1957 i mentors was Faye/e 25 5 EH 955mm J-WZZ' Z Patented Apr. 30, 1940 UNITED STATES PATENT OFFICE WELDED TWO-PIECE Ronald M. Hazen and LIGHT ALLOY PISTON Thomas S. McCrae, Jr..
Indianapolis, Ind., assignors to General Motors Corporation, Detroit,
Delaware Mich., a corporation of 4 Claims.
is twice that of a four-cycle engine and there is approximately twice the waste heat to be dissipated through the parts in a given time. The high thermal conditions not only frequently cause difficulties due to ring sticking, but decrease the strength of the piston to the point where failure may occur.
Accordingly, it is becoming increasingly important to provide pistons which are light, but of adequate strength, while capable of dissipating effectively the heat to which they are subjected.
The object of the invention is a strong, light weight piston, capable of quickly dissipating the 16 heat to which it is subjected.
Another object of the invention is a piston in which the heat flow to the ring belt is limited.
It is a further object of the invention to achieve the foregoing objects in a piston which can be simply and cheaply produced.
The above and other objects of the invention will be apparent as the description proceeds.
According to the invention, the crown of the piston is supported from the piston pin bosses mainly by a circular strut forming an inner wall, spaced from and of greater section than the outer wall of the piston and providing an annular insulating air space between the two walls. The
piston is made in two pieces subsequently fastened together by screwed and/or welded joints, or the like. One piece forms one part of the wall of the annular insulating air space and includes the ring belt area and the strut and the other piece forms the remaining part of the wall of the annular insulating air space and includes the remainder of the piston.
The two-piece construction permits a greater control and freedom in the choice of section and so in the provision of suitable cooling flns and insulating air spaces.
The drawing shows three modifications of a piston according to the invention.
In the drawing: Fig. 1 is a view, partly in elevation andpartly in section, of a piston structure according to the invention.
Figs. 2 and 3 are views, partly in elevation and partly in section of modifications according to the invention.
Referring now to Fig. 1, the piston is provided with diametrically opposite bosses such as I, having bearings 2 for a piston pin (not shown). Integral with the bosses l and above the bosses is a ring b'elt area 3 in which grooves 4 are provided for conventional packing rings (not shown) and a circular strut 5 having an outer diameter such as to leave an annular space 6 between the ring belt area 3 and the strut 5.
The piston crown 1 forms the closure for the upper end of the amiular space 6. It has female threads 8 engaging male threads 9 at the top end of the circular strut 5. The peripheral rim III of the piston crown extends to the top edge ll of the piston skirt above the ring belt area 3.
The piston structure is completed by screwing the two parts together, after which the joint between the rim ll) of the piston crown and the top edge II is sealed by welding as indicated in the drawing.
The construction according to Fig. 2 is essentially similar to the construction according to Fig. 1, except that the circular strut is female threaded and the piston crown is male threaded.
In the modifications according to Fig. 3, the piston crown I5 is integral with the circular strut l6 and the ring belt area l1. The piston skirt portion I8 is a push fit over the bosses I9 which are integral with the circular strut l6 and the ring belt area I! as in the structure according to Fig. 1. The skirt portion I8 is welded to the ring belt area I! as shown.
In all the examples illustrated, the annular space extends closer to the outer cylindrical surface of the piston at points above and below the ring belt area in the outer wall of the piston and has at all points a greater cross-sectional area than points above and below the ring belt area. The heat flow from the head of the piston to the ring belt area is restricted by the narrow section of metal between these two parts. The circular strut forming the inner wall of the insulating annular space is sufficiently large to carry the main gas pressure loads and the heat flow directlyon to the piston pin bosses-only a small part of the load and the heat flow being transmitted through the outer section of the piston.
Because of the lower temperature of the ring belt area, due to the lessened heat flow to this part, the possibility of piston rings sticking, consequent on carbonization of the lubricating oil at the temperature which would otherwise exist, is avoided.
The two parts 01' the piston can be made of any suitable light alloy (either forged or cast), and it will be seen that a structure has been provided in which all critical points, as well as the cooling fins, may be completely machined to any desired tolerance limits before assembl We claim:
1. In a piston having a crown, a slclrt, piston pin bosses, and a ring belt area in the outer wall of the piston between the crown and the piston pin bosses, a strut to support the crown from the piston pin bosses and forming an inner wall spaced from the outer wall of the piston to provide an enclosed annular insulating air space be-. tween the ring belt area and the strut forming the inner wall, said inner wall having at all points a greater cross-sectional area than points above and below the ring belt area inthe outer wall of the piston, whereby only small portions oi the gas pressure loads and the heat to which the crown is exposed in an engine cylinder are transmitted to the ring belt area, and the main portions oi. the gas pressure loads and'the heat flow are carried directly through the inner wall to the piston pin bosses, said piston consisting of v a plurality oi pieces fastened together, one of said pieces forming a part. of the wall of the annular insulating air space and including the ring belt area and the strut, there being a Joint in the outer periphery of the piston above the piston pin bosses, between said piece and the remainder of the piston.
2. The combination according to claim 1, in which the ring belt area and the strut are part of the piece including the skirt.
3. The combination according to claim 1, in
which the ring belt area, the strut and the piston pin bosses are part of the piece including the crown.
4. The combination according to claim 1, in
which the joint in the outer periphery oi the piston above the piston pin bosses is a welded 'joint, and there is an additional screw threaded connection between the two pieces.
RONALD M. HAZEN. THOMAS S. MCCRAE. JR.
US264380A 1937-04-19 1939-03-27 Welded two-piece light alloy piston Expired - Lifetime US2198771A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
US264380A US2198771A (en) 1937-04-19 1939-03-27 Welded two-piece light alloy piston

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
US137656A US2159989A (en) 1937-04-19 1937-04-19 Welded two-piece light alloy piston
US264380A US2198771A (en) 1937-04-19 1939-03-27 Welded two-piece light alloy piston

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US2198771A true US2198771A (en) 1940-04-30

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Cited By (8)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2524369A (en) * 1945-08-22 1950-10-03 Smith Corp A O Method of electric flash welding cylindrical members and product thereof
US2882106A (en) * 1954-06-24 1959-04-14 Maschf Augsburg Nuernberg Ag Piston for internal combustion engines
US4372194A (en) * 1978-03-31 1983-02-08 Regie Nationale Des Usines Renault Internal combustion engine piston
US5642654A (en) * 1994-09-01 1997-07-01 Sundstrand Corporation Piston and method of manufacturing the same
US20060225568A1 (en) * 2003-08-19 2006-10-12 Michael Ullrich Split piston for an internal combustion engine
DE102006027354A1 (en) * 2006-06-13 2007-12-20 Mahle International Gmbh Multi-piece cooled piston for an internal combustion engine
US20110168016A1 (en) * 2007-08-02 2011-07-14 Achim Fedyna Assembled piston
US9127616B2 (en) 2012-10-09 2015-09-08 Federal-Mogul Corporation Piston assembly and method of making a piston

Cited By (10)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2524369A (en) * 1945-08-22 1950-10-03 Smith Corp A O Method of electric flash welding cylindrical members and product thereof
US2882106A (en) * 1954-06-24 1959-04-14 Maschf Augsburg Nuernberg Ag Piston for internal combustion engines
US4372194A (en) * 1978-03-31 1983-02-08 Regie Nationale Des Usines Renault Internal combustion engine piston
US5642654A (en) * 1994-09-01 1997-07-01 Sundstrand Corporation Piston and method of manufacturing the same
US20060225568A1 (en) * 2003-08-19 2006-10-12 Michael Ullrich Split piston for an internal combustion engine
US7311075B2 (en) * 2003-08-19 2007-12-25 Mahle Gmbh Split piston for an internal combustion engine
DE102006027354A1 (en) * 2006-06-13 2007-12-20 Mahle International Gmbh Multi-piece cooled piston for an internal combustion engine
US8201537B2 (en) 2006-06-13 2012-06-19 Mahle International Gmbh Multi-part cooled piston for an internal combustion engine
US20110168016A1 (en) * 2007-08-02 2011-07-14 Achim Fedyna Assembled piston
US9127616B2 (en) 2012-10-09 2015-09-08 Federal-Mogul Corporation Piston assembly and method of making a piston

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